AD 47-02-07
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Superior Aircraft Company | V | Airworthiness Directives; Culver Models V and V2 Aircraft |
| aircraft | Superior Aircraft Company | V-2 | Airworthiness Directives; Culver Models V and V2 Aircraft |
Unsafe Condition
Improper adjustment of the landing gear retraction system could result in damage to the retraction system due to insufficient upward pressure on the retraction links, unequal pressure on the push-pull rods, or improper down limit switch gap settings.
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Required Actions
Inspect the landing gear retraction system every 100 hours of operation to ensure push-pull rod adjustments withstand a minimum upward pressure of 25 pounds, equal pressure on both main gear struts, and down limit switch gap between 0.015 inch to 0.020 inch.
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Compliance Time
after each 100 hours of operation
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Affected Aircraft
Superior Aircraft Company Models V and V2 Aircraft
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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